Deformation analysis of wing structures
The elementary theories of bending and torsion often do not describe the stresses in aircraft shell structures with adequate accuracy; more refined stress theories have therefore have developed over a period of years. Theories of this nature are applied to the problem of calculating the deflections,...
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Main Author: | |
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Corporate Author: | |
Format: | eBook |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1361. |
Subjects: | |
ISBN: | 9781680156072 1680156071 |
Physical Description: | 1 online resource (34 pages, 9 unnumbered pages) : illustrations |
Online Access:
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